FR2563517A1 - METHOD FOR INTRODUCING A LOAD IN A PROJECTILE ENVELOPE - Google Patents
METHOD FOR INTRODUCING A LOAD IN A PROJECTILE ENVELOPE Download PDFInfo
- Publication number
- FR2563517A1 FR2563517A1 FR8506228A FR8506228A FR2563517A1 FR 2563517 A1 FR2563517 A1 FR 2563517A1 FR 8506228 A FR8506228 A FR 8506228A FR 8506228 A FR8506228 A FR 8506228A FR 2563517 A1 FR2563517 A1 FR 2563517A1
- Authority
- FR
- France
- Prior art keywords
- envelope
- charge
- load
- temperature
- introducing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/02—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges
- F42B33/025—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges by compacting
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B21/00—Apparatus or methods for working-up explosives, e.g. forming, cutting, drying
- C06B21/0033—Shaping the mixture
- C06B21/0041—Shaping the mixture by compression
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Press Drives And Press Lines (AREA)
- Agricultural Chemicals And Associated Chemicals (AREA)
Abstract
PROCEDE D'INTRODUCTION D'UNE CHARGE DANS UNE DOUILLE DE PROJECTILE. ON PRECOMPRIME D'ABORD UNE CHARGE EXPLOSIVE A L'EXTERIEUR D'UNE ENVELOPPE, PUIS ON L'INTRODUIT SOUS FORME D'UNE EBAUCHE 5 DANS L'ENVELOPPE 6 ET L'ON EN ACHEVE ENSUITE LA COMPRESSION AVEC UN POINCON 9. POUR OBTENIR UN COMPACTAGE UNIFORME DE LA CHARGE DANS L'ENVELOPPE 6, ON AMENE LA CHARGE A UNE TEMPERATURE INFERIEURE A CELLE DE L'ENVELOPPE 6, APRES LA PRECOMPRESSION. AVANT LA NEUTRALISATION DE CETTE DIFFERENCE DE TEMPERATURE, ON INTRODUIT LA CHARGE DANS L'ENVELOPPE 6. DE PREFERENCE, ON EN ACHEVE LA COMPRESSION ET ON LA FIXE, DANS CELLE-CI, AVANT LA NEUTRALISATION DE LA DIFFERENCE DE TEMPERATURE.METHOD OF INTRODUCING A CHARGE IN A PROJECTILE SOCKET. FIRST PRECOMPRESS AN EXPLOSIVE CHARGE OUTSIDE AN ENVELOPE, THEN WE INSERT IT IN THE FORM OF A BLANK 5 IN ENVELOPE 6 AND THEN COMPLETE THE COMPRESSION WITH A PUNCH 9. TO OBTAIN A UNIFORM COMPACTION OF THE LOAD IN THE ENVELOPE 6, THE LOAD IS BROUGHT TO A TEMPERATURE LOWER THAN THAT OF THE ENVELOPE 6, AFTER PRECOMPRESSION. BEFORE THE NEUTRALIZATION OF THIS TEMPERATURE DIFFERENCE, THE CHARGE IS INTRODUCED IN ENVELOPE 6. PREFERABLY, COMPRESSION IS COMPLETED AND FIXED IN IT BEFORE THE NEUTRALIZATION OF THE TEMPERATURE DIFFERENCE.
Description
Procédé d'introduction d'une charge dans uneMethod of introducing a charge into a
enveloppe de projectile.projectile envelope.
La présente invention concerne un procédé d'in- The present invention relates to a method of
troduction d'une charge dans une enveloppe de projectile, en précomprimant d'abord la charge à l'extérieur de l'enveloppe, puis en l'introduisant dans la douille et en en achevant ensuite la compression. troduction of a charge into a projectile envelope, first precompressing the charge on the outside of the envelope, then introducing it into the socket and then completing the compression.
Un procédé de ce type est décrit dans la DE-A- A process of this type is described in DE-A-
31 07 788.31 07 788.
Lorsqu'on comprime des charges actives de den- When one compresses active loads of den-
sité élevée, il faut appliquer des puissances de compres- high level, it is necessary to apply compro-
sion corrélativement élevées à la charge. Il s'est avéré correspondingly high to the load. It has been found
que, lorsqu'on comprime des charges allongées, le compac- when compressing elongated loads, the compaction
tage dans la zone de la charge opposée au poinçon est plus faible que dans la zone qui en est proche. Cela doit être attribué aux forces de friction internes de the area of the load opposite the punch is lower than in the area near it. This must be attributed to the internal friction forces of
la matière de la charge explosive. De telles hétérogé- the material of the explosive charge. Such heterogeneous
néités de compactage des charges ont des effets fâcheux burden compaction have untoward effects
sur les performances de la charge explosive. on the performance of the explosive charge.
La présente invention a pour objet un procédé du type précité permettant d'obtenir une charge compactée The present invention relates to a method of the aforementioned type for obtaining a compacted charge
(comprimée) uniformément dans l'enveloppe du projectile. (compressed) evenly in the shell of the projectile.
Pour atteindre cet objectif, selon l'invention, To achieve this objective, according to the invention,
à partir d'un procédé du type précité, après la précom- from a process of the type mentioned above, after the precom-
pression de la charge, on l'amène à une température inférieure à celle de l'enveloppe du projectile et l'on pressure of the charge, it is brought to a temperature lower than that of the shell of the projectile and one
introduit la charge dans l'enveloppe avant la neutrali- introduces the charge into the envelope before neutralizing
sation de la différence de température. Grace à la dif- the difference in temperature. Thanks to the difference
férence de température entre l'enveloppe et la charge, le volume de la charge précomprimée est inférieur au temperature difference between the envelope and the load, the volume of the precompressed load is less than
volume de l'enveloppe du projectile destinée à la loger. volume of the shell of the projectile intended to house it.
Lors de la neutralisation de la différence de température When neutralizing the temperature difference
qui a lieu après l'introduction de la charge dans l'en- which takes place after the introduction of the charge into the
veloppe, un compactage de la charge dans l'enveloppe se produit automatiquement. Ainsi, la charge est compactée, même dans les zones qui ne seraient pas compactées de la veloppe, compaction of the load in the envelope occurs automatically. Thus, the charge is compacted, even in areas that would not be compacted from the
même façon par compression.same way by compression.
Du fait que l'enveloppe et la charge précompri- Because the envelope and the precompensated
mée sont amenées à des températures différentes avant are brought to different temperatures before
d'être réunies, la dilatation et la contraction corré- to be united, the dilatation and the contraction
latives facilitent, en outre, l'introduction de la charge dans l'enveloppe. latives facilitate, in addition, the introduction of the load in the envelope.
Selon un mode de réalisation préféré de l'inven- According to a preferred embodiment of the invention,
tion, la compression de la charge est déjà achevée après tion, the compression of the load is already completed after
son introduction dans l'enveloppe, avant la neutralisa- its introduction into the envelope, before the neutralization
tion de la différence de température. De préférence, on fixe ensuite la charge dans l'enveloppe avant la neutralisation de la différence de température. Grâce difference in temperature. Preferably, the charge is then fixed in the envelope prior to the neutralization of the temperature difference. grace
à cette mesure, lors de la neutralisation de la diffé- to this extent, when neutralizing the difference between
rence de température, la charge est déjà fixée mécani- temperature, the load is already mechanically
quement dans l'enveloppe, de sorte que les forces de dilatation et de contraction ont des effets pratiquement only in the envelope, so that the forces of expansion and contraction
complets sur le compactage de la charge. complete on compacting the load.
Selon un mode de réalisation préféré de l'in- According to a preferred embodiment of the invention,
vention, on laisse l'enveloppe à la température ambiante et l'on refroidit la charge par rapport à elle. On ne risque pas, de ce fait, que la charge soit chauffée par In this case, the jacket is left at room temperature and the charge is cooled with respect thereto. As a result, the load is not heated by
une enveloppe préchauffée.a preheated envelope.
On va décrire à présent des formes préféren- We will now describe preferred forms
tielles d'un exemple du procédé selon l'invention, re- of an example of the process according to the invention,
présenté sur le dessin annexé dont les Figures 1 à 5 représentent des étapes opératoires successives du procédé selon l'invention, ou plus précisément: la Figure 1 représente la précompression de la charge; la Figure 2 représente le refroidissement de la charge; la Figure 3 représente l'introduction de la charge dans une enveloppe de projectile; 1 to 5 show successive operating steps of the process according to the invention, or more precisely: FIG. 1 represents the precompression of the charge; Figure 2 shows the cooling of the load; Figure 3 shows the introduction of the charge into a projectile envelope;
la Figure 4 représente l'achèvement du compac- Figure 4 shows the completion of the compaction
tage de la charge dans l'enveloppe; la Figure 5 représente la fixation de la charge dans l'enveloppe; On charge une matière de charge explosive 1 dans un fourreau 3 d'outil de moulage par compression placé sur un poinçon inférieur 2. Ensuite, on appuie un poinçon supérieur 4 contre le poinçon inférieur 2. On obtient ainsi une ébauche 5 dont le volume peut encore être légèrement supérieur au volume intérieur d'une enveloppe de projectile 6 comportant une garniture 7 the load in the envelope; Figure 5 shows the attachment of the load in the envelope; An explosive charge material 1 is loaded into a compression molding tool sleeve 3 placed on a lower punch 2. An upper punch 4 is then pressed against the lower punch 2. This produces a blank 5 whose volume can be adjusted. still be slightly greater than the interior volume of a projectile envelope 6 having a lining 7
(voir Figure 5).(see Figure 5).
Les hétérogénéités de compactage de la matière de charge explosive 1 n'ont pas d'effets gênants dans The heterogeneities of compaction of the explosive charge material 1 do not have any troublesome effects in
l'ébauche 5.the draft 5.
On refroidit l'ébauche 5 dans une chambre de The blank 5 is cooled in a chamber of
refroidissement 8 à environ -30 C (voir Figure 2). cooling 8 at about -30 C (see Figure 2).
Elle se contracte alors. Ensuite, on introduit l'ébauche It contracts then. Then we introduce the draft
contractée 5 dans l'enveloppe 6 et l'on place la garni- contract 5 in the envelope 6 and the packing is
ture 7 sur l'ébauche 5 (voir Figure 3). L'enveloppe 6 Figure 7 on the blank 5 (see Figure 3). The envelope 6
et la garniture 7 sont à la température ambiante. and the liner 7 are at room temperature.
Immédiatement après, on comprime la garniture 7 sur l'ébauche 5 encore refroidie au moyen d'un autre poinçon 9, ceci achevant le compactage de l'ébauche Immediately after, the lining 7 is pressed on the still-cooled blank 5 by means of another punch 9, this completing the compaction of the blank
(voir Figure 4).(see Figure 4).
Ensuite, on visse, dans un taraudage 10 de l'enveloppe 6, une bague de fixation 11 comportant un filetage 12. La bague de fixation 11 appuie la garniture 7 sur l'ébauche 5 encore refroidie (Figure 5). Cela Then, in a tapping 10 of the casing 6, a fixing ring 11 having a thread 12 is screwed. The fixing ring 11 presses the lining 7 onto the still-cooled blank 5 (FIG. 5). it
maintient l'ébauche 5 entre l'enveloppe 6 et le revê- maintains the blank 5 between the envelope 6 and the cover
tement 7.7.
Immédiatement après, la température de l'ébauche formée par la matière de charge explosive i monte à la valeur de la température ambiante de l'enveloppe 6 et de la garniture 7. La dilatation qui en résulte entratne un compactage de la matière de charge explosive 1 de l'ébauche 5, simultané avec le compactage produit Immediately thereafter, the temperature of the blank formed by the explosive charge material i rises to the value of the ambient temperature of the casing 6 and the packing 7. The resulting expansion results in compaction of the explosive charge material. 1 of the blank 5, simultaneous with the compaction produced
par l'achèvement de la compression et s'ajoutant à lui. by the completion of compression and adding to it.
Le résultat final est donc que toutes les zones de la The end result is therefore that all areas of the
matière de charge explosive 1 sont compactées unifor- explosive charge material 1 are compacted uniformly
mément. Le choix de la dilatation et de la contraction dépendant de la différence de température et du jeu entre l'enveloppe 6 et l'ébauche précomprimée 5 permet ance. The choice of expansion and contraction depending on the difference in temperature and the clearance between the envelope 6 and the precompressed preform 5 allows
de déterminer le degré de compactage supplémentaire. to determine the degree of additional compaction.
L'invention ne se limite pas à l'exemple de réalisation décrit. On peut aussi la mettre en oeuvre The invention is not limited to the embodiment described. It can also be implemented
en préchauffant l'enveloppe 6 en plus ou exclusivement. preheating the envelope 6 more or exclusively.
On peut aussi utiliser l'invention lorsqu'on introduit, au lieu de la charge précomprimée en un seul bloc It is also possible to use the invention when introducing, instead of the precompressed feed in a single block
décrite, deux ou plusieurs fractions de charge pré- described, two or more fractions of charge pre-
comprimées dans l'enveloppe 6.compressed in the envelope 6.
Claims (5)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19843415389 DE3415389A1 (en) | 1984-04-25 | 1984-04-25 | METHOD FOR PUTTING A LOAD INTO A FLOOR CASE |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2563517A1 true FR2563517A1 (en) | 1985-10-31 |
FR2563517B1 FR2563517B1 (en) | 1987-10-16 |
Family
ID=6234339
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8506228A Expired FR2563517B1 (en) | 1984-04-25 | 1985-04-24 | METHOD FOR INTRODUCING A LOAD INTO A PROJECTILE ENVELOPE |
Country Status (5)
Country | Link |
---|---|
US (1) | US4651618A (en) |
DE (1) | DE3415389A1 (en) |
FR (1) | FR2563517B1 (en) |
GB (1) | GB2158922B (en) |
NL (1) | NL190065C (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0494469A1 (en) * | 1991-01-11 | 1992-07-15 | Schweizerische Eidgenossenschaft vertreten durch die Eidg. Munitionsfabrik Thun der Gruppe für Rüstungsdienste | Method of assembling a hollow charge |
EP3701215A4 (en) * | 2017-10-26 | 2020-12-16 | Spectra Technologies LLC | Explosive ordnance cold assembly process |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4842061A (en) * | 1988-02-05 | 1989-06-27 | Vetco Gray Inc. | Casing hanger packoff with C-shaped metal seal |
DE3843886C1 (en) * | 1988-12-24 | 1990-05-31 | Dynamit Nobel Ag, 5210 Troisdorf, De | Process for producing main charges and booster charges of hollow charges |
DE3914343A1 (en) * | 1989-04-29 | 1990-10-31 | Messerschmitt Boelkow Blohm | Hollow charge mfr. - by determining internal volume of case before filling in the proper explosive charge for finish pressing |
DE3939295A1 (en) * | 1989-11-28 | 1991-05-29 | Rheinmetall Gmbh | METHOD AND DEVICE FOR PRODUCING LARGE-SCALE AMMUNITION |
US5445513A (en) * | 1994-01-10 | 1995-08-29 | Hitech Holding, Inc. | Apparatus for enhancing concentration |
US5489349A (en) * | 1995-04-06 | 1996-02-06 | Trw Inc. | Grains of gas generating material and process for forming the grains |
KR101028813B1 (en) * | 2009-01-19 | 2011-04-12 | 국방과학연구소 | Method and apparatus for loading cartridges with pressable plastic bonded exposive |
US8136437B2 (en) * | 2010-03-23 | 2012-03-20 | Martin Electronics, Inc. | Modular hand grenade |
US9546856B1 (en) * | 2014-09-22 | 2017-01-17 | The United States Of America As Represented By The Secretary Of The Army | Press load process for warhead |
US11209255B1 (en) | 2019-09-10 | 2021-12-28 | The United States Of America As Represented By The Secretary Of The Army | Press load process for warheads |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE518009A (en) * | ||||
US1978146A (en) * | 1933-11-06 | 1934-10-23 | Rheinische Metallw & Maschf | Method of charging small caliber high explosive shells |
US2960000A (en) * | 1953-09-02 | 1960-11-15 | Commerce Internat Soc Et | Methods for filling shells |
US3472656A (en) * | 1967-02-13 | 1969-10-14 | Oregon Metallurgical Corp | Method of manufacturing articles from particulate metal masses |
DE2239281A1 (en) * | 1972-08-10 | 1974-02-21 | Dynamit Nobel Ag | METHOD OF MANUFACTURING EXPLOSIVES SURROUNDED BY A HULL |
US3931709A (en) * | 1972-03-03 | 1976-01-13 | Societe Nationale Des Poudres Et Explosifs | Method of loading a solid fuel rocket engine |
DE2656310A1 (en) * | 1976-12-11 | 1978-06-15 | Dynamit Nobel Ag | Elongated explosive charges - with separate sticks bonded in thin-walled metal case by self-hardening compound |
GB2038455A (en) * | 1978-12-04 | 1980-07-23 | Dynamit Nobel Ag | Process for the manufacture of compressed explosive bodies |
DE3236706A1 (en) * | 1982-10-04 | 1984-04-05 | Rheinmetall GmbH, 4000 Düsseldorf | Process for lining a body surrounding a cavity and consisting of explosive mixtures with an insert |
Family Cites Families (12)
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---|---|---|---|---|
GB410703A (en) * | 1933-12-13 | 1934-05-24 | Rheinische Metallw & Maschf | Method of charging small calibre high explosive shells |
DE966737C (en) * | 1952-03-20 | 1957-09-05 | Prb Nv | Device for the production of explosive bodies, in particular projectile charges |
DE2035851C3 (en) * | 1970-07-18 | 1979-03-15 | Dynamit Nobel Ag, 5210 Troisdorf | Propellant charge powder body and process for its manufacture |
US3907947A (en) * | 1971-06-24 | 1975-09-23 | Us Navy | Method for shaped charge bomblet production |
FR2240427B1 (en) * | 1973-08-09 | 1976-11-19 | Thomson Brandt | |
US3968724A (en) * | 1974-10-03 | 1976-07-13 | The United States Of America As Represented By The Secretary Of The Army | Method for accurately varying the density of a powder or powder charge, and shrink tubes for use therewith |
US4357856A (en) * | 1976-11-12 | 1982-11-09 | The United States Of America As Represented By The Secretary Of The Navy | Propellant for liquid propellant gun |
SE421346B (en) * | 1977-10-05 | 1981-12-14 | Bofors Ab | METHOD AND DEVICE FOR PRESSING PYROTECHNICAL KITS |
DE2852334A1 (en) * | 1978-12-04 | 1980-06-26 | Dynamit Nobel Ag | METHOD FOR THE PRODUCTION OF PRESSED, IN PARTICULAR LARGE-CALIBRATED COMBUSTION CHARGES |
US4450768A (en) * | 1981-01-12 | 1984-05-29 | Schlumberger Technical Corporation | Shaped charge and method of making it |
DE3107788C2 (en) * | 1981-02-28 | 1982-11-25 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Method and apparatus for producing explosive devices with a main charge and a transfer charge in a casing |
US4495867A (en) * | 1982-06-18 | 1985-01-29 | E. I. Du Pont De Nemours And Company | Assembly for initiating explosives with low-energy detonating cord |
-
1984
- 1984-04-25 DE DE19843415389 patent/DE3415389A1/en active Granted
-
1985
- 1985-02-11 NL NLAANVRAGE8500372,A patent/NL190065C/en not_active IP Right Cessation
- 1985-03-25 US US06/715,505 patent/US4651618A/en not_active Expired - Fee Related
- 1985-04-23 GB GB08510323A patent/GB2158922B/en not_active Expired
- 1985-04-24 FR FR8506228A patent/FR2563517B1/en not_active Expired
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE518009A (en) * | ||||
US1978146A (en) * | 1933-11-06 | 1934-10-23 | Rheinische Metallw & Maschf | Method of charging small caliber high explosive shells |
US2960000A (en) * | 1953-09-02 | 1960-11-15 | Commerce Internat Soc Et | Methods for filling shells |
US3472656A (en) * | 1967-02-13 | 1969-10-14 | Oregon Metallurgical Corp | Method of manufacturing articles from particulate metal masses |
US3931709A (en) * | 1972-03-03 | 1976-01-13 | Societe Nationale Des Poudres Et Explosifs | Method of loading a solid fuel rocket engine |
DE2239281A1 (en) * | 1972-08-10 | 1974-02-21 | Dynamit Nobel Ag | METHOD OF MANUFACTURING EXPLOSIVES SURROUNDED BY A HULL |
DE2656310A1 (en) * | 1976-12-11 | 1978-06-15 | Dynamit Nobel Ag | Elongated explosive charges - with separate sticks bonded in thin-walled metal case by self-hardening compound |
GB2038455A (en) * | 1978-12-04 | 1980-07-23 | Dynamit Nobel Ag | Process for the manufacture of compressed explosive bodies |
DE3236706A1 (en) * | 1982-10-04 | 1984-04-05 | Rheinmetall GmbH, 4000 Düsseldorf | Process for lining a body surrounding a cavity and consisting of explosive mixtures with an insert |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0494469A1 (en) * | 1991-01-11 | 1992-07-15 | Schweizerische Eidgenossenschaft vertreten durch die Eidg. Munitionsfabrik Thun der Gruppe für Rüstungsdienste | Method of assembling a hollow charge |
US5251530A (en) * | 1991-01-11 | 1993-10-12 | Schweizerische Eidenossenschaft Vertreten Durch Die Eidg. Munitionsfabrik Thun Der Gruppe Fur Rustungsdienste | Method for assembling a hollow-charge projectile |
EP3701215A4 (en) * | 2017-10-26 | 2020-12-16 | Spectra Technologies LLC | Explosive ordnance cold assembly process |
Also Published As
Publication number | Publication date |
---|---|
DE3415389C2 (en) | 1989-10-26 |
GB2158922A (en) | 1985-11-20 |
US4651618A (en) | 1987-03-24 |
NL190065C (en) | 1993-10-18 |
GB8510323D0 (en) | 1985-05-30 |
DE3415389A1 (en) | 1985-11-07 |
NL190065B (en) | 1993-05-17 |
GB2158922B (en) | 1988-04-20 |
NL8500372A (en) | 1985-11-18 |
FR2563517B1 (en) | 1987-10-16 |
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